Книги з теми "Composite and sandwich plate"
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Plate and panel structures of isotropic, composite and piezoelectric materials, including sandwich construction. Dordrecht: Springer, 2005.
Знайти повний текст джерелаVinson, Jack R. Plate and Panel Structures of Isotropic, Composite and Piezoelectric Materials, Including Sandwich Construction. Dordrecht: Springer Netherlands, 2005. http://dx.doi.org/10.1007/1-4020-3111-4.
Повний текст джерелаFilho, Mário Kataoka. Optimization of nonhomogeneous facesheets in composite sandwich plates. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1997.
Знайти повний текст джерелаYu, Yi-Yuan. Vibrations of Elastic Plates: Linear and Nonlinear Dynamical Modeling of Sandwiches, Laminated Composites, and Piezoelectric Layers. New York, NY: Springer New York, 1996.
Знайти повний текст джерелаF, Lung S., Gupta K. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаF, Lung S., Gupta K. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A three-node C ̊element for analysis of laminated composite sandwich shells. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаVibrations of elastic plates: Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York: Springer, 1996.
Знайти повний текст джерелаChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаAbrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013.
Знайти повний текст джерелаAbrate, Serge, Bruno Castanié, and Yapa D. S. Rajapakse, eds. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5329-7.
Повний текст джерелаM. J. L. van Tooren. Sandwich fuselage design. Delft, Netherlands: Delft University Press, 1998.
Знайти повний текст джерелаCheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.
Знайти повний текст джерелаLee, Sung W., ed. Advances in Thick Section Composite and Sandwich Structures. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.
Повний текст джерелаDaniel, I. M., E. E. Gdoutos, and Y. D. S. Rajapakse, eds. Major Accomplishments in Composite Materials and Sandwich Structures. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3141-9.
Повний текст джерелаCheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.
Знайти повний текст джерелаAuerkari, Pertti. Effect of impact face damage on strength of sandwich composites. Espoo, Finland: Technical Research Centre of Finland, 1993.
Знайти повний текст джерелаGopalakrishnan, Srinivasan, and Yapa Rajapakse, eds. Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-7170-6.
Повний текст джерелаToledano, A. A composite plate theory for arbitrary laminate configurations. Arlington, Va: Office of Naval Research, 1985.
Знайти повний текст джерелаOskooei, Saeid G. A higher order finite element for sandwich plate analysis. Ottawa: National Library of Canada, 1998.
Знайти повний текст джерелаStorakers, Bertil. Nonlinear plate theory applied to delamination in composites. Stockholm, Sweden: The Royal Institute of Technology, Department of Strength of Materials and Solid Mechanics, 1987.
Знайти повний текст джерелаJungbluth, O. Verbund- und Sandwichtragwerke: Tragverhalten, Feuerwiderstand, Bauphysik. Berlin: Springer-Verlag, 1986.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Optimization of composite sandwich cover panels subjected to compressive loadings. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Знайти повний текст джерелаThe behavior of sandwich structures of isotropic and composite materials. Lancaster, Pa: Technomic Pub. Co., 1999.
Знайти повний текст джерелаD, Vannucci Raymond, and United States. National Aeronautics and Space Administration., eds. Mechanical properties characterization of composite sandwich materials intended for space antenna applications. [Washington, DC: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаCenter, Langley Research, ed. A treatise on equivalent-plate stiffnesses for stiffened laminated-composite plates and plate-like lattices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2011.
Знайти повний текст джерелаCenter, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаCenter, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаR, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.
Знайти повний текст джерелаR, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.
Знайти повний текст джерелаR, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.
Знайти повний текст джерелаC, Marques Elizabeth R., Lee Samson S, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Massachusetts Institute of Technology, and Lewis Research Center, eds. Modes of vibration on square fiberglass epoxy composite thick plate. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаH, Williams James. Modes of vibration on square fiberglass epoxy composite thick plate. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаWalker, Sandra P. Evaluation of composite honeycomb sandwich panels under compressive loads at elevated temperatures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаSomers, M. Effect of delamination location on postbuckling behavior of sandwich structures. Haifa, Israel: Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Знайти повний текст джерелаJegley, Dawn C. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. Hampton, Va: Langley Research Center, 1992.
Знайти повний текст джерелаSomers, M. Buckling and postbuckling behavior of sandwich structures in the presence of a delamination. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Знайти повний текст джерелаNajafi, Ali A. End plate connections and their influence on steel and composite structures. [s.l.]: typescript, 1992.
Знайти повний текст джерелаY, Rajapakse, Kardomateas George A, American Society of Mechanical Engineers. Applied Mechanics Division., and International Mechanical Engineering Congress and Exposition (1999 : Nashville, Tenn.), eds. Thick composites for load bearing structures: Presented at the 1999 ASME International Mechanical Engineering Congress and Exposition, November 14-19, 1999, Nashville, Tennessee. New York: American Society of Mechanical Engineers, 1999.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаMcGowan, David Michael. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаCenter, Langley Research, ed. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаMcGowan, David Michael. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаMcGowan, David Michael. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаCenter, Langley Research, ed. Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаBrown, Nigel D. Aspects of sway frame design and ductility of composite end plate connections. [s.l.]: typescript, 1995.
Знайти повний текст джерелаFacility, Dryden Flight Research, ed. Stress concentration around a small circular hole in the HiMAT composite plate. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Знайти повний текст джерелаKo, William L. Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments. Edwards, Calif: Dryden Flight Research Facility, 1991.
Знайти повний текст джерелаViita-Aho, Tarvo. A finite element analysis of the response of composite sandwich panels to blast loading. Manchester: UMIST, 1992.
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